TY - GEN
T1 - Asymmetric error-constrained path-following control of a stratospheric airship
AU - Chen, Tian
AU - Zhu, Ming
AU - Zheng, Zewei
N1 - Publisher Copyright:
© 2018 Technical Committee on Control Theory, Chinese Association of Automation.
PY - 2018/10/5
Y1 - 2018/10/5
N2 - This paper addresses the asymmetric error-constrained vector filed path-following problem of a stratospheric airship with external disturbances. An algorithm for asymmetric error-constrained path-following of the stratospheric airship is proposed based on the theories of asymmetric barrier Lyapunov function, vector field guidance and adaptive sliding mode control. Firstly, the asymmetric vector field guidance law (AVFGL) is presented, which can navigate the stratospheric airship along the predefined path and guarantee the tracking error is limited by aysmmetric error constriants. Secondly, an adaptive sliding mode attitude controller is introduced to track the desired attitude caculated by the AVFGL. Finally, an adaptive velocity controller to maintain constant velocity is added to the control algrithm. Simulation results demonstrate the effectiveness of the proposed control algorithm.
AB - This paper addresses the asymmetric error-constrained vector filed path-following problem of a stratospheric airship with external disturbances. An algorithm for asymmetric error-constrained path-following of the stratospheric airship is proposed based on the theories of asymmetric barrier Lyapunov function, vector field guidance and adaptive sliding mode control. Firstly, the asymmetric vector field guidance law (AVFGL) is presented, which can navigate the stratospheric airship along the predefined path and guarantee the tracking error is limited by aysmmetric error constriants. Secondly, an adaptive sliding mode attitude controller is introduced to track the desired attitude caculated by the AVFGL. Finally, an adaptive velocity controller to maintain constant velocity is added to the control algrithm. Simulation results demonstrate the effectiveness of the proposed control algorithm.
KW - Asymmetric Error Constraints
KW - Path Following Control
KW - Stratospheric Airship
KW - Vector Field
UR - https://www.scopus.com/pages/publications/85056082057
U2 - 10.23919/ChiCC.2018.8482781
DO - 10.23919/ChiCC.2018.8482781
M3 - 会议稿件
AN - SCOPUS:85056082057
T3 - Chinese Control Conference, CCC
SP - 3932
EP - 3937
BT - Proceedings of the 37th Chinese Control Conference, CCC 2018
A2 - Chen, Xin
A2 - Zhao, Qianchuan
PB - IEEE Computer Society
T2 - 37th Chinese Control Conference, CCC 2018
Y2 - 25 July 2018 through 27 July 2018
ER -